FR2905734B1 - Dispositif permettant d'ameliorer l'efficacite des traitements acoustiques dans un conduit d'une motorisation d'aeronef - Google Patents

Dispositif permettant d'ameliorer l'efficacite des traitements acoustiques dans un conduit d'une motorisation d'aeronef

Info

Publication number
FR2905734B1
FR2905734B1 FR0653606A FR0653606A FR2905734B1 FR 2905734 B1 FR2905734 B1 FR 2905734B1 FR 0653606 A FR0653606 A FR 0653606A FR 0653606 A FR0653606 A FR 0653606A FR 2905734 B1 FR2905734 B1 FR 2905734B1
Authority
FR
France
Prior art keywords
conduit
enhancing
efficiency
aircraft engine
acoustic treatments
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Fee Related
Application number
FR0653606A
Other languages
English (en)
French (fr)
Other versions
FR2905734A1 (fr
Inventor
Fabrice Gantie
Yann Druon
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Airbus Operations SAS
Original Assignee
Airbus Operations SAS
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Priority to FR0653606A priority Critical patent/FR2905734B1/fr
Application filed by Airbus Operations SAS filed Critical Airbus Operations SAS
Priority to BRPI0714746-5A priority patent/BRPI0714746A2/pt
Priority to EP07823777.3A priority patent/EP2069625B1/fr
Priority to CA002661874A priority patent/CA2661874A1/fr
Priority to US12/440,354 priority patent/US8167232B2/en
Priority to CN2007800333116A priority patent/CN101558224B/zh
Priority to JP2009527181A priority patent/JP5058262B2/ja
Priority to PCT/FR2007/051880 priority patent/WO2008029062A2/fr
Priority to RU2009112609/06A priority patent/RU2454556C2/ru
Publication of FR2905734A1 publication Critical patent/FR2905734A1/fr
Application granted granted Critical
Publication of FR2905734B1 publication Critical patent/FR2905734B1/fr
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00—Details, component parts, or accessories
    • F04D29/66—Combating cavitation, whirls, noise, vibration or the like; Balancing
    • F04D29/661—Combating cavitation, whirls, noise, vibration or the like; Balancing especially adapted for elastic fluid pumps
    • F04D29/662—Balancing of rotors
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/24—Heat or noise insulation
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/44—Nozzles having means, e.g. a shield, reducing sound radiation in a specified direction
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/78—Other construction of jet pipes
    • F02K1/82—Jet pipe walls, e.g. liners
    • F02K1/827—Sound absorbing structures or liners
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
    • F02K3/02—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
    • F02K3/04—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2230/00—Manufacture
    • F05D2230/90—Coating; Surface treatment
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2240/00—Components
    • F05D2240/10—Stators
    • F05D2240/12—Fluid guiding means, e.g. vanes
    • F05D2240/126—Baffles or ribs
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2250/00—Geometry
    • F05D2250/30—Arrangement of components
    • F05D2250/33—Arrangement of components symmetrical
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2250/00—Geometry
    • F05D2250/70—Shape
    • F05D2250/71—Shape curved
    • F05D2250/711—Shape curved convex
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2250/00—Geometry
    • F05D2250/70—Shape
    • F05D2250/71—Shape curved
    • F05D2250/712—Shape curved concave
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Soundproofing, Sound Blocking, And Sound Damping (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
FR0653606A 2006-09-07 2006-09-07 Dispositif permettant d'ameliorer l'efficacite des traitements acoustiques dans un conduit d'une motorisation d'aeronef Expired - Fee Related FR2905734B1 (fr)

Priority Applications (9)

Application Number Priority Date Filing Date Title
FR0653606A FR2905734B1 (fr) 2006-09-07 2006-09-07 Dispositif permettant d'ameliorer l'efficacite des traitements acoustiques dans un conduit d'une motorisation d'aeronef
EP07823777.3A EP2069625B1 (fr) 2006-09-07 2007-09-06 Dispositif permettant d'améliorer l'efficacité des traitements acoustiques dans un conduit d'une motorisation d'aéronef
CA002661874A CA2661874A1 (fr) 2006-09-07 2007-09-06 Dispositif permettant d'ameliorer l'efficacite des traitements acoustiques dans un conduit d'une motorisation d'aeronef
US12/440,354 US8167232B2 (en) 2006-09-07 2007-09-06 Device that makes it possible to improve the effectiveness of the acoustic treatments in a pipe of an aircraft power plant
BRPI0714746-5A BRPI0714746A2 (pt) 2006-09-07 2007-09-06 nacela de aeronave e aeronave
CN2007800333116A CN101558224B (zh) 2006-09-07 2007-09-06 用于提高飞行器动力装置腔道中声音处理有效性的设备
JP2009527181A JP5058262B2 (ja) 2006-09-07 2007-09-06 航空機の動力機構のダクト内の音響処理効果を改善する装置
PCT/FR2007/051880 WO2008029062A2 (fr) 2006-09-07 2007-09-06 Dispositif permettant d'améliorer l'efficacité des traitements acoustiques dans un conduit d'une motorisation d'aéronef
RU2009112609/06A RU2454556C2 (ru) 2006-09-07 2007-09-06 Гондола летательного аппарата (варианты) с улучшенной обработкой шумов и летательный аппарат, оснащенный такой гондолой

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0653606A FR2905734B1 (fr) 2006-09-07 2006-09-07 Dispositif permettant d'ameliorer l'efficacite des traitements acoustiques dans un conduit d'une motorisation d'aeronef

Publications (2)

Publication Number Publication Date
FR2905734A1 FR2905734A1 (fr) 2008-03-14
FR2905734B1 true FR2905734B1 (fr) 2012-07-13

Family

ID=37944390

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0653606A Expired - Fee Related FR2905734B1 (fr) 2006-09-07 2006-09-07 Dispositif permettant d'ameliorer l'efficacite des traitements acoustiques dans un conduit d'une motorisation d'aeronef

Country Status (9)

Country Link
US (1) US8167232B2 (ru)
EP (1) EP2069625B1 (ru)
JP (1) JP5058262B2 (ru)
CN (1) CN101558224B (ru)
BR (1) BRPI0714746A2 (ru)
CA (1) CA2661874A1 (ru)
FR (1) FR2905734B1 (ru)
RU (1) RU2454556C2 (ru)
WO (1) WO2008029062A2 (ru)

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GB201007215D0 (en) * 2010-04-30 2010-06-16 Rolls Royce Plc Gas turbine engine
GB201101609D0 (en) * 2011-01-31 2011-03-16 Rolls Royce Plc Attenuation of open rotor noise
US10837367B2 (en) * 2012-02-28 2020-11-17 Raytheon Technologies Corporation Acoustic treatment in an unducted area of a geared turbomachine
US9856745B2 (en) * 2012-02-28 2018-01-02 United Technologies Corporation Acoustic treatment in an unducted area of a geared turbomachine
EP2725196A1 (en) 2012-10-24 2014-04-30 Alstom Technology Ltd Combustor transition
FR3078107B1 (fr) 2018-02-19 2020-07-31 Safran Aircraft Engines Nacelle de turbomachine a parois acoustiquement poreuses
DE102020128400B3 (de) 2020-10-28 2022-01-27 Airbus Defence and Space GmbH Strömungskörper für ein Fahrzeug und Verfahren zum Herstellen eines Strömungskörpers

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US2759554A (en) * 1952-08-04 1956-08-21 Bolt Beranek & Newman Acoustic absorber
US2918984A (en) * 1953-10-08 1959-12-29 Koppers Co Inc Sound control shroud for aircraft engines
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US3002341A (en) * 1957-12-31 1961-10-03 Boeing Co Jet engine noise suppression nozzles
US2990906A (en) * 1958-10-08 1961-07-04 Koppers Co Inc Acoustic absorber
GB1212875A (en) * 1967-12-21 1970-11-18 Rolls Royce Aircraft
US3477231A (en) * 1967-12-26 1969-11-11 Gen Electric Noise reduction
FR1580553A (ru) * 1968-07-26 1969-09-05
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US3533486A (en) * 1968-11-08 1970-10-13 Gen Electric Jet engine silencer with retractable sound absorbing body
US3574477A (en) * 1969-02-19 1971-04-13 Boeing Co Noise attenuating system for rotary engines
GB1284341A (en) * 1970-01-28 1972-08-09 Rolls Royce Fluid flow machine
US3745629A (en) * 1972-04-12 1973-07-17 Secr Defence Method of determining optimal shapes for stator blades
US3890060A (en) 1974-02-15 1975-06-17 Gen Electric Acoustic duct with asymmetric acoustical treatment
US4023644A (en) * 1975-07-02 1977-05-17 The Boeing Company Fluid layer acoustic shield for turbofan jet propulsion engine
US4131387A (en) * 1976-02-27 1978-12-26 General Electric Company Curved blade turbomachinery noise reduction
US4137992A (en) * 1976-12-30 1979-02-06 The Boeing Company Turbojet engine nozzle for attenuating core and turbine noise
US4335801A (en) * 1980-12-15 1982-06-22 The Boeing Company Noise suppressing nozzle
US4817756A (en) * 1985-08-26 1989-04-04 Aeronautic Development Corp. Ltd. Quiet nacelle system and hush kit
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Also Published As

Publication number Publication date
WO2008029062A2 (fr) 2008-03-13
WO2008029062A3 (fr) 2008-05-29
BRPI0714746A2 (pt) 2013-05-14
JP5058262B2 (ja) 2012-10-24
CN101558224A (zh) 2009-10-14
CN101558224B (zh) 2013-10-30
US20100038476A1 (en) 2010-02-18
CA2661874A1 (fr) 2008-03-13
EP2069625B1 (fr) 2019-01-09
RU2009112609A (ru) 2010-10-20
WO2008029062A8 (fr) 2008-04-17
RU2454556C2 (ru) 2012-06-27
EP2069625A2 (fr) 2009-06-17
FR2905734A1 (fr) 2008-03-14
JP2010502885A (ja) 2010-01-28
US8167232B2 (en) 2012-05-01

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Effective date: 20110916

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Effective date: 20110916

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Effective date: 20110913

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